NTSB CAROL · Event
Event ATL05CA151
Registry · N262T
FAA Aircraft Registry record.
Make / Model
PIPER PA-18 105
Year of manufacture
1953 · 52 years old at event
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19560523
ADS-B equipped
Yes — Mode-S A28814
Registrant of record
BARNSTORMERS AERIAL ADVERTISING LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power due to the pilot's failure to use carburetor heat, which resulted in the formation of carburetor ice.
Factual narrative
On August 22, 2005, at 1615 eastern daylight time, a Piper PA-18-105, N262T, registered to and operated by Barnstormer Flite Signs Inc, collided with the Atlantic Ocean at North Myrtle Beach, South Carolina. The banner tow flight was operated under the provisions of Title 14 CFR Part 91 and no flight plan was filed. Visual meteorological conditions prevailed at the time of the accident. The pilot was not injured, and the airplane received substantial Damage. The flight departed Grand Stand Airport, North Myrtle Beach, South Carolina, at 1330 August 22, 2005. The pilot departed Grand Stand Airport on a routine banner tow flight around the North Myrtle Beach area. The airplane had flown for about two and a half hours and was at an altitude of 500 feet when engine started to run rough. The engine continued to run rough for 45-60 seconds followed by the engine completely losing power. The pilot's attempts to restart the engine were unsuccessful and the pilot chose to ditch the airplane in the Atlantic Ocean. The airplane was ditched 125 yards from the coast and was recovered by witnesses at the scene of the accident. Post accident-examination of the airplane revealed saltwater throughout the engine and engine accessories. Saltwater was drained from the recovered engine and the engine was started and a functional run was accomplished. The pilot stated there was 15 gallons of fuel in the left fuel tank and 5 gallons remaining in the right fuel tank when he ditched the airplane. Weather conditions were favorable for the formation of carburetor ice. The pilot reported that he did not apply carburetor heat during the flight. The pilot departed Grand Stand Airport on a routine banner tow flight around the North Myrtle Beach area. The airplane had flown for about two and a half hours and was at an altitude of 500 feet when the engine started to run rough. The engine continued to run rough for 45-60 seconds followed by the engine completely losing power. The pilot's attempts to restart the engine were unsuccessful and the pilot chose to ditch the airplane in the Atlantic Ocean. The airplane was ditched 125 yards from the coast and was recovered by witnesses at the scene of the accident. Post accident-examination of the airplane revealed saltwater throughout the engine and engine accessories. Saltwater was drained from the recovered engine and the engine was started and a functional run was accomplished. According to carburetor icing charts, weather conditions were favorable for the formation of carburetor ice. The pilot reported that he did not apply carburetor heat during the flight. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_ATL05CA151.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗